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Priority to KR1019910004041ApriorityCriticalpatent/KR920018315A/en
Publication of KR920018315ApublicationCriticalpatent/KR920018315A/en
Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like
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Abstract
내용 없음No content
Description
동력발생장치Power generator
본 내용은 요부공개 건이므로 전문내용을 수록하지 않았음Since this is an open matter, no full text was included.
제1도는 본 발명의 구성을 나타내는 계통도,1 is a system diagram showing the configuration of the present invention,
제2도는 본 발명중 기체분사구를 나타내는 평면도,2 is a plan view showing a gas injection port in the present invention,
제3도는 본 발명중 임펠러의 구조를 나타내는 사시도.Figure 3 is a perspective view showing the structure of the impeller in the present invention.
Claims (1)
동력을 발생시키는 동력발생장치에 있어서, 주연료통(1)과 연결되고 액체상태의 연료를 기체상태의 연료로 상태 변화시키며, 기체상태의 연료를 압축시키기 위한 열은 제공하는 예열구(6)를 포함하는 연료가열통(4)과; 상기 연료가열통(4)의 좌우측에 위치하여 연료의 상태변화와 압축 과정에서 상기 연료가열통(4)의 체적을 일정하게 유지시키기 위한 제1, 제2압력밸브(17,18)와; 상기 연료가열통(4)과 연결된 가스압력통(8)과 연결되어 고압 기체 상태인 연료를 회전축(12)에 고정된 임펠러(10)에 분사하는 기체분사구(9)와; 상기 기체분사구(9)로 분사된 기체를 주연료봉(1)에 이송시키기 위해 기체상태의 연료를 액체상태로 상태변화시키기 위한 냉각구조(15)로 된 것을 특징으로 하는 동력발생장치.In a power generating device for generating power, a preheating port (6) connected to the main fuel container (1) and converting a liquid fuel into a gaseous fuel and providing heat for compressing the gaseous fuel is provided. A fuel heating cylinder 4 including; First and second pressure valves 17 and 18 positioned on the left and right sides of the fuel heating tube 4 to maintain a constant volume of the fuel heating tube 4 during a state change and compression of the fuel; A gas injection hole (9) connected to the gas pressure cylinder (8) connected to the fuel heating cylinder (4) to inject a fuel in a high pressure gas state to the impeller (10) fixed to the rotary shaft (12); And a cooling structure (15) for changing a gaseous fuel into a liquid state in order to transfer the gas injected into the gas injection port (9) to the main fuel rod (1).※ 참고사항 : 최초출원 내용에 의하여 공개하는 것임.※ Note: The disclosure is based on the initial application.
Supersonic combustion studies. 2- Exponential relationships between pressure, area and process length, for heat addition in a non-constant-area duct(Gas dynamic equations based on injection and combustion of gaseous fuels in supersonic flow of high enthalpy air flowing in non-constant area combustion chamber)